# STC SA378SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerial Repairing
- Description: Installation of Lycoming O-320 engine
- Status date: November 1, 1965
- Data sheets: A-797, A-780
- Certificate PDF: https://openairdocs.org/files/sha256/29/0b/290b7d8e50e34eca44ff53d68a763bf0c8f957ab30e569e497caaacfc65de79a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3AC7F68E58040F2C86257DC400575F3E.0001
- Page: https://openairdocs.org/stc/SA378SW

## ADs that name it

None.

## Approved models (2)

- FS 2002 Corp. PA-14 (TCDS A-797)
- FS 2003 Corp. PA-12 (TCDS A-780)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

**FEDERAL AVIATION AGENCY**

**SUPPLEMENTAL TYPE CERTIFICATE FORM APPROVED, BUDGET BUREAU NO. 04-R015**

**INSTRUCTIONS - SUBMIT IN TRI PLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.**

**COPY WILL BE RETURNED TO APPLICANT UPON**

**ISSUANCE**

1. NAME AND ADDRESS OF APPLICANT V. L. Olaetaad Aerial Repairing P. 0. Box 909 Ponca City, Oklahoma

2. SUPPLEMENTAL TYPE CERTIFICATE APPLIED FOR:

I——I AlRCRAFT ENGINE PROPELLER

ORIGINAL MODEL DESIGNATION PA«ia anA PA-1A NEW MODEL DESIGNATION (If demired) ————————none————————3. DESCRIPTION OF CHANGE Installation of LyeoAing 0*320 engine per Installation Instructions and parts List dated 1/16/63 and drawings listed thereon. Installation of 6 inch wheel* per Drawing WM-100 dated 1/16/64. Installation of Piper PA-18 horizontal tail surfaces per Installation Instructions dated 1/16/64.

MOTES: 1. FAA approved Airplane Flight Manual Supplement dated 4/28/64 required for the Piper PA-14 aircraft.

2. FAA Approved Airplane Flight Manual Supplement dated 10/28/65 required for the Piper PA-12 aircraft.

. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? £] YES CD NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Kef. CAR 1.55)1 StU YES I1 NO

**5. SIGNATURE AND TITLE OF APPLICANT**

**SIGNATURE**

**DATE OF APPLICATION TITLE**

6. To be Completed by FAA

NATURE AND LOCATION OF DATA Data listed in Item 3 above and Conformity Inspection Reports dated 5/7/64 and 1/22/65 on file at 3W-210.

Reference Project: A2413WS Applicable regulations: same as original certification.

**ORIGINAL TYPE CERTIFICATE NO.**

**780 6 797 SUPPLEMENTAL TYPE CERTIFICATE NO.**

SA378SW

DATE OF APPROVAL 5/7/64 Revision 1 11/1/65

**FAA APPROVAL**

SIGNATURE H. H. Slaughter Chief, Engineering and Manufacturing BranchTl TLE * U.S. GOVERNMENT PRINTING OFFICE : 1959 0—509657 FORM FAA-2417 (5-59)

## Every issue (1)

- November 1, 1965: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/29/0b/290b7d8e50e34eca44ff53d68a763bf0c8f957ab30e569e497caaacfc65de79a)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.